EP3036404A4 - Agencement de turbine à section variable à modulation de flux secondaire - Google Patents
Agencement de turbine à section variable à modulation de flux secondaire Download PDFInfo
- Publication number
- EP3036404A4 EP3036404A4 EP14837668.4A EP14837668A EP3036404A4 EP 3036404 A4 EP3036404 A4 EP 3036404A4 EP 14837668 A EP14837668 A EP 14837668A EP 3036404 A4 EP3036404 A4 EP 3036404A4
- Authority
- EP
- European Patent Office
- Prior art keywords
- secondary flow
- variable area
- turbine arrangement
- flow modulation
- area turbine
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
- F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
- F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
- F01D11/20—Actively adjusting tip-clearance
- F01D11/24—Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
- F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/06—Fluid supply conduits to nozzles or the like
- F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/205—Cooling fluid recirculation, i.e. after cooling one or more components is the cooling fluid recovered and used elsewhere for other purposes
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP21174516.1A EP3907374A1 (fr) | 2013-08-21 | 2014-08-13 | Agencement de turbine à zone variable avec modulation d'écoulement secondaire |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201361868121P | 2013-08-21 | 2013-08-21 | |
PCT/US2014/050862 WO2015026597A1 (fr) | 2013-08-21 | 2014-08-13 | Agencement de turbine à section variable à modulation de flux secondaire |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP21174516.1A Division EP3907374A1 (fr) | 2013-08-21 | 2014-08-13 | Agencement de turbine à zone variable avec modulation d'écoulement secondaire |
Publications (3)
Publication Number | Publication Date |
---|---|
EP3036404A1 EP3036404A1 (fr) | 2016-06-29 |
EP3036404A4 true EP3036404A4 (fr) | 2017-03-22 |
EP3036404B1 EP3036404B1 (fr) | 2021-05-19 |
Family
ID=52484052
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP14837668.4A Active EP3036404B1 (fr) | 2013-08-21 | 2014-08-13 | Agencement de turbine à section variable à modulation de flux secondaire |
EP21174516.1A Pending EP3907374A1 (fr) | 2013-08-21 | 2014-08-13 | Agencement de turbine à zone variable avec modulation d'écoulement secondaire |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP21174516.1A Pending EP3907374A1 (fr) | 2013-08-21 | 2014-08-13 | Agencement de turbine à zone variable avec modulation d'écoulement secondaire |
Country Status (3)
Country | Link |
---|---|
US (2) | US10132191B2 (fr) |
EP (2) | EP3036404B1 (fr) |
WO (1) | WO2015026597A1 (fr) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10094229B2 (en) | 2014-07-28 | 2018-10-09 | United Technologies Corporation | Cooling system of a stator assembly for a gas turbine engine having a variable cooling flow mechanism and method of operation |
US10253648B2 (en) | 2016-03-04 | 2019-04-09 | General Electric Company | Modulated hybrid variable area turbine nozzle for gas turbine engine |
US10358934B2 (en) * | 2016-04-11 | 2019-07-23 | United Technologies Corporation | Method and apparatus for adjusting variable vanes |
US10352182B2 (en) | 2016-05-20 | 2019-07-16 | United Technologies Corporation | Internal cooling of stator vanes |
US10739002B2 (en) | 2016-12-19 | 2020-08-11 | General Electric Company | Fluidic nozzle assembly for a turbine engine |
US10711640B2 (en) * | 2017-04-11 | 2020-07-14 | Raytheon Technologies Corporation | Cooled cooling air to blade outer air seal passing through a static vane |
US10436050B2 (en) | 2017-04-11 | 2019-10-08 | United Technologies Corporation | Guide vane arrangement for gas turbine engine |
US11060463B2 (en) * | 2018-01-08 | 2021-07-13 | Raytheon Technologies Corporation | Modulated combustor bypass and combustor bypass valve |
US10480322B2 (en) * | 2018-01-12 | 2019-11-19 | General Electric Company | Turbine engine with annular cavity |
US10619509B2 (en) | 2018-04-27 | 2020-04-14 | United Technologies Corporation | Gas turbine engine flow modulation in a rotating vane |
US11668202B2 (en) * | 2018-08-06 | 2023-06-06 | Raytheon Technologies Corporation | Airfoil core inlets in a rotating vane |
US11021962B2 (en) * | 2018-08-22 | 2021-06-01 | Raytheon Technologies Corporation | Turbulent air reducer for a gas turbine engine |
GB201818063D0 (en) * | 2018-11-06 | 2018-12-19 | Rolls Royce Plc | An actuation system |
CN110043328B (zh) * | 2018-12-17 | 2021-10-22 | 中国航发沈阳发动机研究所 | 一种冷却式变几何低压涡轮导向叶片 |
FR3108362B1 (fr) * | 2020-03-19 | 2022-07-29 | Safran Aircraft Engines | Etage d’aubes à orientation variable pour une turbomachine axiale comprenant un organe de régulation du débit d’air dépendant de l’orientation des aubes |
FR3108656B1 (fr) * | 2020-03-24 | 2022-03-04 | Safran Aircraft Engines | Dispositif de refroidissement et de pressurisation d'une turbine de turbomachine. |
CN116557349B (zh) * | 2023-05-18 | 2024-05-17 | 中国船舶集团有限公司第七〇三研究所 | 一种双层交错式压气机机匣处理结构 |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20030223856A1 (en) * | 2002-05-30 | 2003-12-04 | Mitsubishi Heavy Industries, Ltd. | Gas turbine and method of bleeding gas therefrom |
US20100202873A1 (en) * | 2009-02-06 | 2010-08-12 | General Electric Company | Ceramic Matrix Composite Turbine Engine |
US20120093632A1 (en) * | 2010-10-15 | 2012-04-19 | General Electric Company | Variable turbine nozzle system |
US20130031913A1 (en) * | 2011-08-02 | 2013-02-07 | Little David A | Movable strut cover for exhaust diffuser |
Family Cites Families (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3314654A (en) | 1965-07-30 | 1967-04-18 | Gen Electric | Variable area turbine nozzle for axial flow gas turbine engines |
GB1067930A (en) * | 1965-12-29 | 1967-05-10 | Rolls Royce | Vane operating mechanism for fluid flow machines |
US3471126A (en) * | 1966-10-31 | 1969-10-07 | United Aircraft Corp | Movable vane unit |
US3663118A (en) * | 1970-06-01 | 1972-05-16 | Gen Motors Corp | Turbine cooling control |
US3850544A (en) * | 1973-11-02 | 1974-11-26 | Gen Electric | Mounting arrangement for a bearing of axial flow turbomachinery having variable pitch stationary blades |
US4169692A (en) * | 1974-12-13 | 1979-10-02 | General Electric Company | Variable area turbine nozzle and means for sealing same |
US4025227A (en) | 1975-06-30 | 1977-05-24 | United Technologies Corporation | Variable area turbine |
US4193738A (en) * | 1977-09-19 | 1980-03-18 | General Electric Company | Floating seal for a variable area turbine nozzle |
US4187054A (en) * | 1978-04-20 | 1980-02-05 | General Electric Company | Turbine band cooling system |
US4741667A (en) | 1986-05-28 | 1988-05-03 | United Technologies Corporation | Stator vane |
GB2210935B (en) * | 1987-10-10 | 1992-05-27 | Rolls Royce Plc | Variable stator vane assembly |
US5683225A (en) | 1991-10-28 | 1997-11-04 | General Electric Company | Jet engine variable area turbine nozzle |
US5517817A (en) * | 1993-10-28 | 1996-05-21 | General Electric Company | Variable area turbine nozzle for turbine engines |
US7628579B2 (en) * | 2005-07-20 | 2009-12-08 | United Technologies Corporation | Gear train variable vane synchronizing mechanism for inner diameter vane shroud |
US7690889B2 (en) * | 2005-07-20 | 2010-04-06 | United Technologies Corporation | Inner diameter variable vane actuation mechanism |
FR2913052B1 (fr) * | 2007-02-22 | 2011-04-01 | Snecma | Commande des aubes a angle de calage variable |
US8007229B2 (en) | 2007-05-24 | 2011-08-30 | United Technologies Corporation | Variable area turbine vane arrangement |
US8202043B2 (en) * | 2007-10-15 | 2012-06-19 | United Technologies Corp. | Gas turbine engines and related systems involving variable vanes |
EP2058524A1 (fr) * | 2007-11-12 | 2009-05-13 | Siemens Aktiengesellschaft | Compresseur à purge d'air doté de conduits dans les aubes variables |
US8393857B2 (en) | 2009-10-09 | 2013-03-12 | Rolls-Royce Corporation | Variable vane actuation system |
EP3090146B8 (fr) * | 2013-11-25 | 2021-04-07 | Raytheon Technologies Corporation | Procédé pour amener un liquide de refroidissement sur une surface portante mobile |
FR3051219B1 (fr) * | 2016-05-12 | 2019-06-07 | Safran Aircraft Engines | Aube de turbomachine, telle par exemple qu'un turboreacteur ou un turbopropulseur d'avion |
US10718229B2 (en) * | 2016-07-21 | 2020-07-21 | Rolls-Royce North American Technologies, Inc. | Infrared suppression system in a gas turbine engine |
BE1024982B1 (fr) * | 2017-02-09 | 2018-09-10 | Safran Aero Boosters Sa | Compresseur de turbomachine avec aubes a calage variable |
US10450890B2 (en) * | 2017-09-08 | 2019-10-22 | Pratt & Whitney Canada Corp. | Variable stator guide vane system |
US11668202B2 (en) * | 2018-08-06 | 2023-06-06 | Raytheon Technologies Corporation | Airfoil core inlets in a rotating vane |
-
2014
- 2014-08-13 WO PCT/US2014/050862 patent/WO2015026597A1/fr active Application Filing
- 2014-08-13 US US14/912,476 patent/US10132191B2/en active Active
- 2014-08-13 EP EP14837668.4A patent/EP3036404B1/fr active Active
- 2014-08-13 EP EP21174516.1A patent/EP3907374A1/fr active Pending
-
2018
- 2018-10-16 US US16/161,593 patent/US10815819B2/en active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20030223856A1 (en) * | 2002-05-30 | 2003-12-04 | Mitsubishi Heavy Industries, Ltd. | Gas turbine and method of bleeding gas therefrom |
US20100202873A1 (en) * | 2009-02-06 | 2010-08-12 | General Electric Company | Ceramic Matrix Composite Turbine Engine |
US20120093632A1 (en) * | 2010-10-15 | 2012-04-19 | General Electric Company | Variable turbine nozzle system |
US20130031913A1 (en) * | 2011-08-02 | 2013-02-07 | Little David A | Movable strut cover for exhaust diffuser |
Non-Patent Citations (1)
Title |
---|
See also references of WO2015026597A1 * |
Also Published As
Publication number | Publication date |
---|---|
WO2015026597A1 (fr) | 2015-02-26 |
EP3036404B1 (fr) | 2021-05-19 |
US10132191B2 (en) | 2018-11-20 |
EP3907374A1 (fr) | 2021-11-10 |
EP3036404A1 (fr) | 2016-06-29 |
US20190048739A1 (en) | 2019-02-14 |
US10815819B2 (en) | 2020-10-27 |
US20160201491A1 (en) | 2016-07-14 |
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